Evaluation des performances d'un design d'avion de type blended-wing-body de 100 passagers

ANNEXE II

APPROCHE CLASSIQUE DE DESIGN CONCEPTUELLE D'UN AÉRONEF

Figure-A II-Schéma du design conceptuel d'un aéronef, basé sur les travaux de
Anderson (2001) et Raymer (2006) (Velazquez, 2020)

120

Figure-A III- Positions tridimensionnelles des profils de design du BWB (Velazquez, 2020)

ANNEXE III

POSITION DES PROFILS DE DESIGN DU BWB (Velazquez, 2020)

121

ANNEXE IV

VISUALISATION DU DESIGN DU BWB AVEC MOTEURS À L'ARRIÈRE DU

FUSELAGE

Figure-A IV-1 Vues de face, de l'arrière et de la gauche du BWB, configuration « moteurs à l'arrière du fuselage »

122

Figure-A IV-2 Multi-vue du BWB, configuration « moteurs à l'arrière du fuselage »

ANNEXE V

Figure-A V-1 Vues de face, de dessus et de l'arrière du BWB, configuration « moteurs sous

l'aile »

VISUALISATION DU DESIGN DU BWB AVEC MOTEURS SOUS L'AILE

124

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	s^'			<--------` '

Figure-A V-2 Multi-vue du BWB, configuration « moteurs sous l'aile »

Howe, D. (2000). Aircraft Conceptual Design Synthesis. Professional Engineering Publishing Limited, London and Bury ST Edmunds, UK, 2000.

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